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GB9306719D0 - A turbine assembly for a gas turbine engine - Google Patents

A turbine assembly for a gas turbine engine

Info

Publication number
GB9306719D0
GB9306719D0 GB939306719A GB9306719A GB9306719D0 GB 9306719 D0 GB9306719 D0 GB 9306719D0 GB 939306719 A GB939306719 A GB 939306719A GB 9306719 A GB9306719 A GB 9306719A GB 9306719 D0 GB9306719 D0 GB 9306719D0
Authority
GB
United Kingdom
Prior art keywords
turbine
assembly
gas turbine
engine
turbine engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
GB939306719A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB939306719A priority Critical patent/GB9306719D0/en
Publication of GB9306719D0 publication Critical patent/GB9306719D0/en
Priority to EP94301535A priority patent/EP0618349A1/en
Pending legal-status Critical Current

Links

GB939306719A 1993-03-31 1993-03-31 A turbine assembly for a gas turbine engine Pending GB9306719D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB939306719A GB9306719D0 (en) 1993-03-31 1993-03-31 A turbine assembly for a gas turbine engine
EP94301535A EP0618349A1 (en) 1993-03-31 1994-03-03 A turbine assembly for a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB939306719A GB9306719D0 (en) 1993-03-31 1993-03-31 A turbine assembly for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB9306719D0 true GB9306719D0 (en) 1993-06-02

Family

ID=10733080

Family Applications (1)

Application Number Title Priority Date Filing Date
GB939306719A Pending GB9306719D0 (en) 1993-03-31 1993-03-31 A turbine assembly for a gas turbine engine

Country Status (2)

Country Link
EP (1) EP0618349A1 (en)
GB (1) GB9306719D0 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0844369B1 (en) * 1996-11-23 2002-01-30 ROLLS-ROYCE plc A bladed rotor and surround assembly
US6227800B1 (en) * 1998-11-24 2001-05-08 General Electric Company Bay cooled turbine casing
DE10122464C1 (en) 2001-05-09 2002-03-07 Mtu Aero Engines Gmbh Mantle ring for low pressure turbine stage of gas turbine uses segments each having seal carrier and relatively spaced security element with minimum contact between them
FR2829176B1 (en) * 2001-08-30 2005-06-24 Snecma Moteurs STATOR CASING OF TURBOMACHINE
FR2846997B1 (en) * 2002-11-07 2006-12-22 Snecma Moteurs ARRANGEMENT FOR MOUNTING RECTIFIER SECTORS
EP2518278A1 (en) 2011-04-28 2012-10-31 Siemens Aktiengesellschaft Turbine casing cooling channel with cooling fluid flowing upstream
ES2620482T3 (en) 2012-08-09 2017-06-28 MTU Aero Engines AG Waterproofing the flow channel of a turbomachine machine
ES2723784T3 (en) 2012-10-23 2019-09-02 MTU Aero Engines AG Cooling air guide in a housing structure of a turbomachine
GB2533544B (en) 2014-09-26 2017-02-15 Rolls Royce Plc A shroud segment retainer
ES2723400T3 (en) 2015-12-07 2019-08-27 MTU Aero Engines AG Housing structure of a turbomachine with thermal protection screen
US10975721B2 (en) 2016-01-12 2021-04-13 Pratt & Whitney Canada Corp. Cooled containment case using internal plenum
CN109339873B (en) * 2018-09-30 2022-01-14 东方电气集团东方汽轮机有限公司 Steam turbine last-stage blade protection device for high back pressure heat supply

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB721453A (en) * 1951-10-19 1955-01-05 Vickers Electrical Co Ltd Improvements relating to gas turbines
GB856599A (en) * 1958-06-16 1960-12-21 Gen Motors Corp Improvements relating to axial-flow compressors
US3335483A (en) * 1961-12-19 1967-08-15 Gen Electric Method of manufacturing a stator assembly for turbomachines
GB2239678B (en) * 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
DE69205568T2 (en) * 1991-04-02 1996-04-11 Rolls Royce Plc TURBINE HOUSING.
US5167488A (en) * 1991-07-03 1992-12-01 General Electric Company Clearance control assembly having a thermally-controlled one-piece cylindrical housing for radially positioning shroud segments

Also Published As

Publication number Publication date
EP0618349A1 (en) 1994-10-05

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